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Effects of Cryogenic Treatment on the Residual Stress and Mechanical Properties of an Aerospace Aluminum AlloyInvestigators at Marshall Space Flight Center (MSFC) are studying the potential benefits of cryogenic treatment for aerospace Aluminum (Al) alloys. This paper reports the effects of cryogenic treatment on residual stress, tensile strength, hardness, fatigue life, and stress corrosion cracking (SCC) resistance.
Document ID
20010067299
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Chen, P. (IIT Research Inst. Huntsville, AL United States)
Malone, T. (NASA Marshall Space Flight Center Huntsville, AL United States)
Bond, R. (IIT Research Inst. Huntsville, AL United States)
Torres, P. (NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
August 20, 2013
Publication Date
February 1, 2001
Publication Information
Publication: Proceedings of The 4th Conference on Aerospace Materials, Processes, and Environmental Technology
Subject Category
Metals And Metallic Materials
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle20010067226Collected WorksProceedings of the 4th Conference on Aerospace Materials, Processes, and Environmental Technology20010067226Collected WorksProceedings of the 4th Conference on Aerospace Materials, Processes, and Environmental Technology
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